发明名称 |
GAS TURBINE ENGINE WITH TIE SHAFT FOR AXIAL HIGH PRESSURE COMPRESSOR ROTOR |
摘要 |
A compressor section to be mounted in a gas turbine engine has a plurality of axial compressor rotors arranged from an upstream location toward a downstream location. A tie shaft applies an axial force at one end of the compressor section and biases the compressor rotors against a hub at the opposite end. The downstream compressor is an axial compressor rotor. A gas turbine engine incorporating this structure is also claimed.
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申请公布号 |
US2011219781(A1) |
申请公布日期 |
2011.09.15 |
申请号 |
US20100720720 |
申请日期 |
2010.03.10 |
申请人 |
BENJAMIN DANIEL;ST MARY CHRISTOPHER;KAPSZUKIEWICZ DANIEL R;LUND BRIAN C |
发明人 |
BENJAMIN DANIEL;ST. MARY CHRISTOPHER;KAPSZUKIEWICZ DANIEL R.;LUND BRIAN C. |
分类号 |
F02C7/20;F04D29/00 |
主分类号 |
F02C7/20 |
代理机构 |
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代理人 |
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主权项 |
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地址 |
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